Bolt-joint structural health monitoring by the method of electromechanical impedance

Author： Pavelko Igor   Pavelko Vitalijs   Kuznetsov Sergey   Ozolinsh Ilmars  

Publisher： Emerald Group Publishing Ltd

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.86, Iss.3, 2014-04, pp. : 207-214

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Related content

The Geometry of a Structural Joint

By Allen C.F.  

Aircraft Engineering, Vol. 17, Iss. 9, 1993-12 ,pp. : 257-258

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Programme Load Fatigue Tests: Evaluation of Aircraft Structural Joint Lives

By A.M.I.Mech.E. R.J. Ryman  

Aircraft Engineering, Vol. 34, Iss. 2, 1993-12 ,pp. : 34-42

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Helicopter Health Monitoring Using an Adaptive Estimator

By Alkahe Jonathan   Rand Omri   Oshman Yaakov  

Journal of the American Helicopter Society, Vol. 48, Iss. 3, 2003-07 ,pp. : 199-210

AHS International

Access to resources Recommend Favorite

Integrated Health and Usage Monitoring System (IHUMS)

By  

Aircraft Engineering, Vol. 64, Iss. 2, 1993-12 ,pp. : 12-15

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Coupled Rotor/Airframe Vibration Analysis by a Combined Harmonic-Balance, Impedance-Matching Method

By Hsu T-K   Peters D. A.  

Journal of the American Helicopter Society, Vol. 27, Iss. 1, 1982-01 ,pp. : 25-34

AHS International

Access to resources Recommend Favorite